FR2005028A1 - - Google Patents

Info

Publication number
FR2005028A1
FR2005028A1 FR6908856A FR6908856A FR2005028A1 FR 2005028 A1 FR2005028 A1 FR 2005028A1 FR 6908856 A FR6908856 A FR 6908856A FR 6908856 A FR6908856 A FR 6908856A FR 2005028 A1 FR2005028 A1 FR 2005028A1
Authority
FR
France
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Pending
Application number
FR6908856A
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Raytheon Technologies Corp
Original Assignee
United Aircraft Corp
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by United Aircraft Corp filed Critical United Aircraft Corp
Publication of FR2005028A1 publication Critical patent/FR2005028A1/fr
Pending legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C9/00Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
    • F02C9/26Control of fuel supply
    • F02C9/28Regulating systems responsive to plant or ambient parameters, e.g. temperature, pressure, rotor speed
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2270/00Control
    • F05D2270/01Purpose of the control system
    • F05D2270/04Purpose of the control system to control acceleration (u)

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Control Of Turbines (AREA)
  • Output Control And Ontrol Of Special Type Engine (AREA)
FR6908856A 1968-03-29 1969-03-28 Pending FR2005028A1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US71713568A 1968-03-29 1968-03-29

Publications (1)

Publication Number Publication Date
FR2005028A1 true FR2005028A1 (fr) 1969-12-05

Family

ID=24880844

Family Applications (1)

Application Number Title Priority Date Filing Date
FR6908856A Pending FR2005028A1 (fr) 1968-03-29 1969-03-28

Country Status (4)

Country Link
US (1) US3513899A (fr)
DE (1) DE1915824C3 (fr)
FR (1) FR2005028A1 (fr)
GB (1) GB1250702A (fr)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2509375A1 (fr) * 1981-07-08 1983-01-14 Snecma Limiteur de deceleration, notamment pour une turbomachine

Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3646753A (en) * 1970-04-28 1972-03-07 United Aircraft Corp Engine compressor bleed control system
US3688504A (en) * 1970-11-27 1972-09-05 Gen Electric Bypass valve control
US3953967A (en) * 1975-03-18 1976-05-04 United Technologies Corporation Servoed throttle valve for fuel controls
US3975903A (en) * 1975-03-18 1976-08-24 United Technologies Corporation Fuel control
US4186556A (en) * 1975-05-29 1980-02-05 General Electric Company Compressor bleed biased acceleration schedule
US4060980A (en) * 1975-11-19 1977-12-06 United Technologies Corporation Stall detector for a gas turbine engine
US4117668A (en) * 1975-11-19 1978-10-03 United Technologies Corporation Stall detector for gas turbine engine
US4128995A (en) * 1976-10-18 1978-12-12 General Electric Company Method and apparatus for stabilizing an augmenter system
US4793133A (en) * 1983-10-28 1988-12-27 Colt Industries Inc Manual backup for electronic fuel control
US5245245A (en) * 1992-05-04 1993-09-14 Motorola, Inc. Mass-loaded cantilever vibrator
US10487752B2 (en) * 2015-03-11 2019-11-26 Pratt & Whitney Canada Corp. Overthrust protection system and method
US11174757B2 (en) 2020-01-20 2021-11-16 Raytheon Technologies Corporation Externally replaceable valve assembly for a turbine engine

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2978166A (en) * 1957-05-28 1961-04-04 Gen Motors Corp Compressor bleed control
US2970435A (en) * 1957-11-27 1961-02-07 Westinghouse Electric Corp Compressor flow control mechanism
US3115006A (en) * 1958-04-21 1963-12-24 United Aircraft Corp Afterburner fuel control
US3091080A (en) * 1958-10-27 1963-05-28 United Aircraft Corp Control system for afterburning gas turbine engine
US3080712A (en) * 1959-02-05 1963-03-12 Continental Aviat & Eng Corp Compressor anti-surge control for a gas turbine engine
US3006145A (en) * 1959-10-14 1961-10-31 Gen Motors Corp Antisurge control using compressor bleed
US3172259A (en) * 1962-03-02 1965-03-09 Avco Corp Variable geometry control for gas turbine engines
US3267670A (en) * 1963-12-13 1966-08-23 Bendix Corp Gas turbine engine control

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2509375A1 (fr) * 1981-07-08 1983-01-14 Snecma Limiteur de deceleration, notamment pour une turbomachine
EP0070229A1 (fr) * 1981-07-08 1983-01-19 Societe Nationale D'etude Et De Construction De Moteurs D'aviation, "S.N.E.C.M.A." Limiteur de décélération dans un régulateur pour une turbomachine
US4503670A (en) * 1981-07-08 1985-03-12 S.N.E.C.M.A. Deceleration limiter, particularly for a turbine engine

Also Published As

Publication number Publication date
GB1250702A (fr) 1971-10-20
DE1915824B2 (de) 1974-01-03
US3513899A (en) 1970-05-26
DE1915824C3 (de) 1974-08-01
DE1915824A1 (de) 1969-10-30

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